FR2990725B1 - METHOD FOR MONITORING A DEGRADATION OF AN AIRCRAFT DEVICE OF AN AIRCRAFT WITH AUTOMATIC DETERMINATION OF A DECISION THRESHOLD - Google Patents
METHOD FOR MONITORING A DEGRADATION OF AN AIRCRAFT DEVICE OF AN AIRCRAFT WITH AUTOMATIC DETERMINATION OF A DECISION THRESHOLDInfo
- Publication number
- FR2990725B1 FR2990725B1 FR1254506A FR1254506A FR2990725B1 FR 2990725 B1 FR2990725 B1 FR 2990725B1 FR 1254506 A FR1254506 A FR 1254506A FR 1254506 A FR1254506 A FR 1254506A FR 2990725 B1 FR2990725 B1 FR 2990725B1
- Authority
- FR
- France
- Prior art keywords
- aircraft
- degradation
- monitoring
- decision threshold
- automatic determination
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B23/00—Testing or monitoring of control systems or parts thereof
- G05B23/02—Electric testing or monitoring
- G05B23/0205—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults
- G05B23/0218—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults characterised by the fault detection method dealing with either existing or incipient faults
- G05B23/0224—Process history based detection method, e.g. whereby history implies the availability of large amounts of data
- G05B23/0227—Qualitative history assessment, whereby the type of data acted upon, e.g. waveforms, images or patterns, is not relevant, e.g. rule based assessment; if-then decisions
- G05B23/0235—Qualitative history assessment, whereby the type of data acted upon, e.g. waveforms, images or patterns, is not relevant, e.g. rule based assessment; if-then decisions based on a comparison with predetermined threshold or range, e.g. "classical methods", carried out during normal operation; threshold adaptation or choice; when or how to compare with the threshold
-
- G—PHYSICS
- G07—CHECKING-DEVICES
- G07C—TIME OR ATTENDANCE REGISTERS; REGISTERING OR INDICATING THE WORKING OF MACHINES; GENERATING RANDOM NUMBERS; VOTING OR LOTTERY APPARATUS; ARRANGEMENTS, SYSTEMS OR APPARATUS FOR CHECKING NOT PROVIDED FOR ELSEWHERE
- G07C5/00—Registering or indicating the working of vehicles
- G07C5/08—Registering or indicating performance data other than driving, working, idle, or waiting time, with or without registering driving, working, idle or waiting time
- G07C5/0808—Diagnosing performance data
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D2045/0085—Devices for aircraft health monitoring, e.g. monitoring flutter or vibration
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Alarm Systems (AREA)
- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
- Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)
- Emergency Alarm Devices (AREA)
- Testing And Monitoring For Control Systems (AREA)
Priority Applications (8)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1254506A FR2990725B1 (en) | 2012-05-16 | 2012-05-16 | METHOD FOR MONITORING A DEGRADATION OF AN AIRCRAFT DEVICE OF AN AIRCRAFT WITH AUTOMATIC DETERMINATION OF A DECISION THRESHOLD |
| US14/401,265 US9346558B2 (en) | 2012-05-16 | 2013-05-15 | Method for monitoring a degradation of an on-board device of an aircraft with automatic determination of a decision threshold |
| CA2873689A CA2873689C (en) | 2012-05-16 | 2013-05-15 | Method for monitoring a degradation of an on-board device of an aircraft with automatic determination of a decision threshold |
| EP13727295.1A EP2850499B1 (en) | 2012-05-16 | 2013-05-15 | Method for monitoring a degradation of an on-board device of an aircraft with automatic determination of a decision threshold |
| RU2014148343A RU2629479C2 (en) | 2012-05-16 | 2013-05-15 | Method of aircraft onboard unit wear control with automatic determination of decision threshold |
| CN201380025537.7A CN104303122B (en) | 2012-05-16 | 2013-05-15 | By automatically determining the method that decision threshold monitors aircraft airborne ageing equipment |
| PCT/FR2013/051059 WO2013171427A1 (en) | 2012-05-16 | 2013-05-15 | Method for monitoring a degradation of an on-board device of an aircraft with automatic determination of a decision threshold |
| BR112014028184A BR112014028184B8 (en) | 2012-05-16 | 2013-05-15 | Process of monitoring a degradation of an aircraft integrated device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1254506A FR2990725B1 (en) | 2012-05-16 | 2012-05-16 | METHOD FOR MONITORING A DEGRADATION OF AN AIRCRAFT DEVICE OF AN AIRCRAFT WITH AUTOMATIC DETERMINATION OF A DECISION THRESHOLD |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2990725A1 FR2990725A1 (en) | 2013-11-22 |
| FR2990725B1 true FR2990725B1 (en) | 2014-05-02 |
Family
ID=48577130
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR1254506A Active FR2990725B1 (en) | 2012-05-16 | 2012-05-16 | METHOD FOR MONITORING A DEGRADATION OF AN AIRCRAFT DEVICE OF AN AIRCRAFT WITH AUTOMATIC DETERMINATION OF A DECISION THRESHOLD |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US9346558B2 (en) |
| EP (1) | EP2850499B1 (en) |
| CN (1) | CN104303122B (en) |
| BR (1) | BR112014028184B8 (en) |
| CA (1) | CA2873689C (en) |
| FR (1) | FR2990725B1 (en) |
| RU (1) | RU2629479C2 (en) |
| WO (1) | WO2013171427A1 (en) |
Families Citing this family (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR3022997B1 (en) | 2014-06-25 | 2016-06-10 | Snecma | METHOD OF MONITORING A DEGRADATION OF AN AIRCRAFT DEVICE OF AN AIRCRAFT INCLUDING THE DETERMINATION OF A COUNTING THRESHOLD |
| FR3027417B1 (en) * | 2014-10-20 | 2016-11-25 | Airbus Operations Sas | METHOD AND SYSTEM FOR GENERATING ALERT REPORTS IN AN AIRCRAFT |
| FR3028067B1 (en) * | 2014-11-05 | 2016-12-30 | Snecma | VALIDATION TOOL FOR A SYSTEM FOR MONITORING AN AIRCRAFT ENGINE |
| JP6649182B2 (en) * | 2016-05-30 | 2020-02-19 | 日本電信電話株式会社 | Probability density function estimation device, continuous value prediction device, method, and program |
| US10373474B2 (en) * | 2017-03-09 | 2019-08-06 | Keithley Instruments, Llc | Auto setting of alarm limits |
| RU2665142C1 (en) * | 2017-08-22 | 2018-08-28 | Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" | Method of flight diagnostics of units of turbofan engine with flow mixing |
| RU2680945C1 (en) * | 2018-04-17 | 2019-02-28 | Закрытое акционерное общество "Туполев-Проект" | Intelligent system of finding failures on aircraft |
| RU2729110C1 (en) * | 2019-07-01 | 2020-08-04 | Акционерное общество "Туполев-Проект" | Intelligent aircraft maintenance system |
| CN112100037B (en) * | 2020-09-25 | 2023-07-25 | 北京奇艺世纪科技有限公司 | Alarm level identification method, device, electronic equipment and storage medium |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| JP3186866B2 (en) * | 1992-11-20 | 2001-07-11 | 株式会社東芝 | Method and apparatus for predicting deterioration / damage of structural member |
| JPH1055497A (en) * | 1996-08-09 | 1998-02-24 | Yazaki Corp | Failure prediction method, control unit and load control system using the same |
| GB9704843D0 (en) * | 1997-03-08 | 1997-04-23 | Murphy Graham F | Apparatus |
| GB9910938D0 (en) * | 1999-05-11 | 1999-07-14 | Murphy Graham F | Diagnostic apparatus |
| US6532421B2 (en) * | 2000-04-07 | 2003-03-11 | Toho Gas Co., Ltd | Method for estimating a life of apparatus under narrow-band random stress variation |
| JP3850311B2 (en) * | 2002-02-21 | 2006-11-29 | オムロン株式会社 | Remaining life prediction notification method and electronic device |
| US6892163B1 (en) * | 2002-03-08 | 2005-05-10 | Intellectual Assets Llc | Surveillance system and method having an adaptive sequential probability fault detection test |
| US7451021B2 (en) * | 2003-05-06 | 2008-11-11 | Edward Wilson | Model-based fault detection and isolation for intermittently active faults with application to motion-based thruster fault detection and isolation for spacecraft |
| US7440811B2 (en) * | 2004-09-28 | 2008-10-21 | Siemens Aktiengesellschaft | Dynamic-state waiting time analysis method for complex discrete manufacturing |
| US7243042B2 (en) * | 2004-11-30 | 2007-07-10 | Siemens Power Generation, Inc. | Engine component life monitoring system and method for determining remaining useful component life |
| US7280941B2 (en) * | 2004-12-29 | 2007-10-09 | General Electric Company | Method and apparatus for in-situ detection and isolation of aircraft engine faults |
| RU2308069C2 (en) * | 2005-06-30 | 2007-10-10 | Валентин Афанасьевич Сухолитко | Method of integrated logistic support of flying vehicle operational monitoring |
| US7933754B2 (en) * | 2006-12-07 | 2011-04-26 | General Electric Company | System and method for damage propagation estimation |
| US7809513B2 (en) * | 2007-04-16 | 2010-10-05 | Acellent Technologies, Inc. | Environmental change compensation in a structural health monitoring system |
| US8437904B2 (en) * | 2007-06-12 | 2013-05-07 | The Boeing Company | Systems and methods for health monitoring of complex systems |
| US20090030752A1 (en) * | 2007-07-27 | 2009-01-29 | General Electric Company | Fleet anomaly detection method |
| US20100030519A1 (en) * | 2008-07-31 | 2010-02-04 | Collier Jarrell D | System for Real-Time Object Damage Detection and Evaluation |
| GB0818544D0 (en) * | 2008-10-09 | 2008-11-19 | Oxford Biosignals Ltd | Improvements in or relating to multi-parameter monitoring |
| US8442702B2 (en) * | 2008-10-22 | 2013-05-14 | Airbus Operations Gmbh | Fault diagnosis device and method for optimizing maintenance measures in technical systems |
| JP5025676B2 (en) * | 2009-03-25 | 2012-09-12 | 株式会社東芝 | Monitoring device and monitoring method |
| CN101963937B (en) * | 2010-09-29 | 2016-08-10 | 南京航空航天大学 | Predicting residual service life of flight control computer system |
| RU2431175C1 (en) * | 2010-10-18 | 2011-10-10 | Федеральное государственное унитарное предприятие "Летно-исследовательский институт имени М.М. Громова" | System for integral monitoring of operation of aircraft onboard equipment |
| CN102288412B (en) * | 2011-05-04 | 2013-05-01 | 哈尔滨工业大学 | Aeroengine hardware damage analysis and service life prediction method based on damage base line |
| GB2491564A (en) * | 2011-05-24 | 2012-12-12 | Isis Innovation | Method of system monitoring |
| FR2989499B1 (en) * | 2012-04-12 | 2014-05-16 | Airbus Operations Sas | METHOD, DEVICES AND COMPUTER PROGRAM FOR PREVENTIVE DIAGNOSTIC ASSISTANCE OF A SYSTEM OF AN AIRCRAFT USING REDUCED EVENT GRAPHICS |
| FR2989500B1 (en) * | 2012-04-12 | 2014-05-23 | Airbus Operations Sas | METHOD, DEVICES AND COMPUTER PROGRAM FOR AIDING THE TROUBLE TOLERANCE ANALYSIS OF AN AIRCRAFT SYSTEM USING REDUCED EVENT GRAPHICS |
| FR2991485B1 (en) * | 2012-06-05 | 2015-08-14 | Airbus Operations Sas | METHOD AND APPARATUS FOR AUTOMATIC ESTIMATING OF CONSUMER AND AIRCRAFT DEGRADATION OF AN AIRCRAFT |
| GB201215649D0 (en) * | 2012-09-03 | 2012-10-17 | Isis Innovation | System monitoring |
| US9014918B2 (en) * | 2012-10-12 | 2015-04-21 | Cummins Inc. | Health monitoring systems and techniques for vehicle systems |
| US9251502B2 (en) * | 2012-11-01 | 2016-02-02 | Ge Aviation Systems Llc | Maintenance system for aircraft fleet and method for planning maintenance |
| US20140257716A1 (en) * | 2013-03-11 | 2014-09-11 | Board Of Trustees Of Michigan State University | Methods for estimating remaining life of a monitored structure |
-
2012
- 2012-05-16 FR FR1254506A patent/FR2990725B1/en active Active
-
2013
- 2013-05-15 CN CN201380025537.7A patent/CN104303122B/en active Active
- 2013-05-15 CA CA2873689A patent/CA2873689C/en active Active
- 2013-05-15 WO PCT/FR2013/051059 patent/WO2013171427A1/en not_active Ceased
- 2013-05-15 RU RU2014148343A patent/RU2629479C2/en active
- 2013-05-15 EP EP13727295.1A patent/EP2850499B1/en active Active
- 2013-05-15 US US14/401,265 patent/US9346558B2/en active Active
- 2013-05-15 BR BR112014028184A patent/BR112014028184B8/en active IP Right Grant
Also Published As
| Publication number | Publication date |
|---|---|
| US20150134198A1 (en) | 2015-05-14 |
| CN104303122A (en) | 2015-01-21 |
| FR2990725A1 (en) | 2013-11-22 |
| EP2850499A1 (en) | 2015-03-25 |
| RU2629479C2 (en) | 2017-08-29 |
| BR112014028184B1 (en) | 2021-02-09 |
| WO2013171427A1 (en) | 2013-11-21 |
| EP2850499B1 (en) | 2016-11-23 |
| CA2873689C (en) | 2020-08-18 |
| RU2014148343A (en) | 2016-07-10 |
| CA2873689A1 (en) | 2013-11-21 |
| BR112014028184B8 (en) | 2022-02-22 |
| BR112014028184A2 (en) | 2017-06-27 |
| US9346558B2 (en) | 2016-05-24 |
| CN104303122B (en) | 2016-09-21 |
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Legal Events
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| CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170717 |
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